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or reverse the thrust if the sonar altitude is less than the [BRAK
ALT].During the brake period, the E9 port of AP outputs a 1800us PWM
signal. After the plane stops or braking time (4 seconds)is up it restores
to 1000us.
The menu item[AUTO LANDING-> Landing Angle] is used to define the
attack angle for touchdown in LND 3/4 stage. In LND 3/4 stage when the
airspeed of the aircraft is greater than[AUTO LANDING-> LANDING
SPEED], the AP flies with a 0 degree attack angle. As the speed of the
plane decreases, the attack angle will automatically increase
progressively. At a speed of 35km/h the attack angle reaches the value
defined by the user.
WARNING: In LND 1/2/3 stages of the landing, once the THR stick on the
transmitter is moved to a position greater than 50%, the plane
temporarily enters STB mode. The mode switches of the transmitter are
still in positions of RTH combination. The mode switch doesn't match the
flying mode until you re-switch it.
The RUNWAY-SCAN Function:
The aforementioned automatic landing process is highly dependent on
the barometer. Circling around L4, approaching L3, and descending to L2
and ready to turn-off the engine. These actions rely on the barometer. If
the barometric altimeter reading is higher than the actual altitude, the